摘要
针对现行有效的14 CFR中Part33有关发动机吞鸟和Part25有关飞机鸟撞的适航规章,分析和对比了相关规章的发展历史、实施范畴和实施重点,掌握了相关规章的内涵和外延,根据规章中验证方法的内容和特点,揭示了相关规章的设置目的、验证方法、设备需求等关键技术问题,梳理了相应技术体系,提出了可借鉴的通用适航符合性分析方法与流程。
The development history,the implementation category and the implementation focus of the relevant regulations were analyzed and compared with respect to the current valid 14 CFR airworthiness regulations of part 33 related to engine bird ingestion and Part25 related to the aircraft bird impact.The connotation and extension of the relevant regulations were mastered.According to the contents and characteristics of the verification method in the regulations,the key technology problems such as the setting purpose,the verification method and the equipment demand of the relevant regulations were revealed,the corresponding technical system was sorted out,and the applicable general airworthiness analysis method and process could be used for reference.
作者
罗刚
张海洋
吴春波
陈伟
丁振东
LUO Gang;ZHANG Hai-yang;WU Chun-bo;CHEN Wei;DING Zhen-dong(College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;Key Laboratory of Impact Dynamics on Aero Engine,Liaoning Province,AECC Shenyang Engine Research Institute,Shenyang 110015,China)
出处
《航空发动机》
北大核心
2019年第6期90-96,共7页
Aeroengine
基金
国家自然科学基金(51575262、51475227)资助
关键词
吞鸟
鸟撞
适航
通用分析方法
航空发动机
bird ingestion
bird impact
airworthiness
general analysis method
aeroengine
